CN209465579U - The full-automatic draw machining center of full SERVO CONTROL - Google Patents
The full-automatic draw machining center of full SERVO CONTROL Download PDFInfo
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- CN209465579U CN209465579U CN201821984438.8U CN201821984438U CN209465579U CN 209465579 U CN209465579 U CN 209465579U CN 201821984438 U CN201821984438 U CN 201821984438U CN 209465579 U CN209465579 U CN 209465579U
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Abstract
The utility model relates to the technical fields of machining equipment, especially a kind of full-automatic draw machining center of full SERVO CONTROL, with fuselage, the waist opens up open slot along its length, the open slot both ends are symmetrically arranged the first driving motor and the second driving motor, and the first driving motor output end and the second driving motor output end are separately connected the first lead screw；Pipe-reduction mold is connected by thread bush on first lead screw, waist setting is located between the pipe-reduction mold and is held down assembly；The fuselage side also sets up loading assemblies, and blanking component is arranged in the fuselage other side.The structure of the complete full-automatic draw machining center of SERVO CONTROL is simple, and primary feed may be implemented, and draw processing and forming, shortening draw process time improve the efficiency of the draw simultaneously at a both ends, guarantee draw quality, convenient for being widely popularized and using.
Description
Technical field
The utility model relates to the technical field of machining equipment, especially a kind of full-automatic draw of full SERVO CONTROL adds
Work center.
Background technique
With the continuous development of society, mechanical processing industry has obtained quick development.Product is carried out plus is processed a bit
There are many mode, and wherein the draw is important component part.The draw is the procedure shunk to tubing products diameter.Tradition
The draw generally use machine for shrinking, run using hydraulic control, but find usually tubing products be made to occur after long-term use
The phenomenon that evaporating, emitting, dripping or leaking of liquid or gas, the serious processing quality for affecting pipe fitting；And current machine for shrinking can only also be carried out for single head
The draw can only carry out the secondary draw, cause the whole draw inefficient in this way when needing the double end draw, it has not been convenient to
Necking operation while people's sight realizes double end simultaneously.
Summary of the invention
Technical problem to be solved by the utility model is: providing one to solve the problems, such as above-mentioned background technique
The complete full-automatic draw machining center of SERVO CONTROL of kind, structure is simple, and primary feed, the draw molding simultaneously of a both ends may be implemented
Draw process time is shortened in processing, improves the efficiency of the draw, guarantees draw quality, convenient for being widely popularized and using.
The technical scheme adopted by the utility model to solve the technical problem is as follows: a kind of full-automatic draw of full SERVO CONTROL adds
Work center has fuselage, and the waist opens up open slot along its length, and the open slot both ends are respectively symmetrically set
The first driving motor and the second driving motor are set, the first driving motor output end and the second driving motor output end are distinguished
Connect the first lead screw；Pipe-reduction mold is connected by thread bush on first lead screw, is located at fuselage between the pipe-reduction mold
Middle part setting holds down assembly；The fuselage side also sets up loading assemblies；Blanking component is arranged in the fuselage other side.
Specifically, described to hold down assembly including guide post, upper pressure seat, down pressing seat, upper and lower clamping platform, upper and lower motor and second
Lead screw；The guide post is vertically set on fuselage, and the guide post upper end is fixed by horizontally disposed clamping platform up and down, institute
The motor up and down stated is vertically set on clamping platform upper end up and down, and second lead screw is vertically plugged in motor side up and down, institute
The second lead screw stated passes through the fixed upper pressure seat in clamping platform rear end up and down from top to bottom, and the down pressing seat is fixed at pressure
The lower section of seat, such design is fixed during the draw to processed pipe fitting to realize.
It further limits, in above-mentioned technical proposal, the two sides of the open slot are located on fuselage upper surface along length
Direction also sets up guide rail, and the pipe-reduction mold lower end two sides pass through the first sliding block and are slidably arranged on guide rail, can be improved
The guiding role of pipe-reduction mold guarantees the accuracy of draw position.
It further limits, in above-mentioned technical proposal, the side of the guide rail, which is located on fuselage end face, to be also fixedly installed
Magnetostrictive displacement sensor, it is such design be in order to guarantee during carrying out the draw, the essence of pipe-reduction mold shift position
Really control.
Specifically, the loading assemblies include crossbeam, connector, fixed block, feeding flat-removing air cyclinder and the first claw；Institute
The crossbeam stated is fixed on guide post in parallel up and down, and the connector is fixed between crossbeam, the connector
Lower end fixed by fixed block, the feeding flat-removing air cyclinder is horizontally set on lower end of fixing block, and first claw is solid
The output end of feeding flat-removing air cyclinder is set calmly, the clamping feeding for being processed pipe fitting may be implemented.
Specifically, the blanking component includes fixed beam, blanking flat-removing air cyclinder, link block and the second claw；Described
Fixed beam is horizontally fixed on guide post, and the blanking flat-removing air cyclinder level is fixed at fixed beam lower end, the blanking
Flat-removing air cyclinder lower end is fixedly connected with block, and the second claw is fixedly installed in the link block side, and such design is to realize
To the folder removal piece of the pipe fitting of completion of processing.
It further limits, in above-mentioned technical proposal, the down pressing seat lower end is slidably arranged in by the second sliding block is led
On rail, the adjustment that the position of down pressing seat may be implemented is fixed.
It further limits, in above-mentioned technical proposal, gyro black assembly is also set up below the loading assemblies, it is described
Gyro black assembly includes turning motor, articulated arm and revolution claw；The turning motor is fixed on fuselage side wall, described
The fixed articulated arm of turning motor output end, the fixed revolution claw in the end of the articulated arm may be implemented in loading assemblies
The supply of pipe fitting.
It further limits, in above-mentioned technical proposal, the gyro black assembly side is located at one middle side part of fuselage and also sets up
Unloader, such design are the fast supplies in order to meet the pipe fitting of whole machine for shrinking.
The beneficial effects of the utility model are: the utility model proposes the full-automatic draw machining center of full SERVO CONTROL,
Structure is simple, primary feed may be implemented, draw processing and forming, shortening draw process time improve the draw simultaneously at a both ends
Efficiency, guarantee draw quality, convenient for being widely popularized and using.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only
It is some embodiments as described in this application, for those of ordinary skill in the art, before not making the creative labor
It puts, is also possible to obtain other drawings based on these drawings.
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the side structure schematic diagram of the utility model；
Fig. 3 is the structural schematic diagram of loading assemblies and blanking component in the utility model；
Fig. 4 is the structural schematic diagram of gyro black assembly in the utility model.
Label in attached drawing are as follows: 1, fuselage；2, open slot；3, the first driving motor；4, the second driving motor；5, first
Thick stick；6, thread bush；7, pipe-reduction mold；8, guide post；9, upper pressure seat；10, down pressing seat；11, upper and lower clamping platform；12, upper and lower motor；
13, the second lead screw；14, guide rail；15, magnetostrictive displacement sensor；16, crossbeam；17, connector；18, fixed block；19, feeding
Flat-removing air cyclinder；20, the first claw；21, fixed beam；22, blanking flat-removing air cyclinder；23, link block；24, the second claw；25, it turns round
Motor；26, articulated arm；27, claw is turned round；28, unloader.
Specific embodiment
The technical issues of in order to keep the utility model solved, technical solution and beneficial effect are more clearly understood, below
In conjunction with accompanying drawings and embodiments, the present invention will be further described in detail.It should be appreciated that specific implementation described herein
Example is only used to explain the utility model, is not used to limit the utility model.
In the description of the present invention, it should be understood that term " side ", " other side ", " two sides ", " between ",
The orientation or positional relationship of the instructions such as " middle part ", " upper end ", " lower end " is to be based on the orientation or positional relationship shown in the drawings, and is only
For ease of description the utility model and simplify description, rather than the device or element of indication or suggestion meaning must have it is specific
Orientation, be constructed and operated in a specific orientation, therefore should not be understood as limiting the present invention.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " is set
Set ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
It, can also be indirectly connected through an intermediary to be to be connected directly.It for the ordinary skill in the art, can be specific
Situation understands the concrete meaning of above-mentioned term in the present invention.
See described in Fig. 1~4 it is the full-automatic draw machining center of full SERVO CONTROL, there is fuselage 1,1 middle part of fuselage is along length
Degree direction opens up open slot 2, and 2 both ends of open slot are symmetrically arranged the first driving motor 3 and the second driving motor 4, and first drives
Dynamic 3 output end of motor and 4 output end of the second driving motor are separately connected the first lead screw 5；Pass through thread bush 6 on first lead screw 5
Pipe-reduction mold 7 is connected, is arranged in the middle part of fuselage 1 between pipe-reduction mold 7 and holds down assembly；1 side of fuselage also sets up loading assemblies；
Blanking component is arranged in 1 other side of fuselage.
Wherein, it holds down assembly including guide post 8, upper pressure seat 9, down pressing seat 10, upper and lower clamping platform 11, upper and lower motor 12 and second
Lead screw 13；Guide post 8 is vertically arranged on the fuselage 1, and 8 upper end of guide post is fixed by horizontally disposed clamping platform 11 up and down, power-on and power-off
Machine 12 is vertically set on 11 upper end of clamping platform up and down, and the second lead screw 13 is vertically plugged in 12 side of motor up and down, the second lead screw 13
The fixed upper pressure seat 9 in upper and lower 11 rear end of clamping platform is passed through from top to bottom, and down pressing seat 10 is fixed at the lower section of upper pressure seat 9.It opens
The two sides of mouthful slot 2 are located on 1 upper surface of fuselage also sets up guide rail 14 along its length, and 7 lower end two sides of pipe-reduction mold pass through the
One sliding block is slidably arranged on guide rail 14.The side of guide rail 14, which is located on 1 end face of fuselage, is also fixedly installed magnetostrictive displacement biography
Sensor 15.Loading assemblies include crossbeam 16, connector 17, fixed block 18, feeding flat-removing air cyclinder 19 and the first claw 20；Crossbeam 16
It is fixed on guide post 8 in parallel up and down, connector 17 is fixed between crossbeam 16, and the lower end of connector 17 passes through fixation
Block 18 is fixed, and feeding flat-removing air cyclinder 19 is horizontally set on 18 lower end of fixed block, and the first claw 20 is fixed at feeding translation gas
The output end of cylinder 19.Blanking component includes fixed beam 21, blanking flat-removing air cyclinder 22, link block 23 and the second claw 24；Fixed beam
21 are horizontally fixed on guide post 8, and 22 level of blanking flat-removing air cyclinder is fixed at 21 lower end of fixed beam, under blanking flat-removing air cyclinder 22
End is fixedly connected with block 23, and the second claw 24 is fixedly installed in 23 side of link block.10 lower end of down pressing seat is set by the sliding of the second sliding block
It sets on guide rail 14.Gyro black assembly is also set up below loading assemblies, gyro black assembly includes turning motor 25, articulated arm 26 and returns
Turn claw 27；Turning motor 25 is fixed on 1 side wall of fuselage, the fixed articulated arm 26 of 25 output end of turning motor, articulated arm
The fixed revolution claw 27 in 26 end.Gyro black assembly side is located at 1 one middle side part of fuselage and also sets up unloader 28.
See figure and Fig. 2, the up and down motion to hold down assembly is to run by upper and lower motor 12, so that upper and lower motor 12 is defeated
Outlet with driving gear you and connect the rotation to drive the second lead screw 13, to realize the up and down motion of upper pressure seat 9；Folder up and down
It is connected through a screw thread between tight platform 11 and the second screw rod 13.
See that Fig. 4, gyro black assembly are fixed on 1 side wall of fuselage by fixed plate, the working principle of gyro black assembly are as follows: first
First, it controls articulated arm 26 by peripheral control unit to rotate downwards, after articulated arm 26 is downward, the revolution claw 27 of end is to
Pipe fitting in place is grabbed, and is then controlled turning motor 25 and is rotated, and the rotation of articulated arm 26 is delivered up to loading assemblies.
See Fig. 3, the operating principle of loading assemblies and blanking component is as follows: firstly, passing through the first card of peripheral control unit control
The pipe fitting of the crawl revolution of pawl 20 27 upper end of claw, is then run by control feeding flat-removing air cyclinder 19, by 20 upper tube of the first claw
Part is pushed in down pressing seat 9；The operating principle of blanking component are as follows: blanking flat-removing air cyclinder 22 is controlled by peripheral control unit and is run to
The position of down pressing seat 10 realizes the clamping to the pipe fitting processed by the second claw 24, controls blanking flat-removing air cyclinder 22
After contraction, pipe fitting is taken out.
In this application, the first driving motor 3, the second driving motor 4, upper and lower motor 12, pipe-reduction mold 7, magnetostriction
Displacement sensor 15, guide rail 14, turning motor 25, unloader 28, feeding flat-removing air cyclinder 19 and blanking flat-removing air cyclinder 22 are all roots
According to concrete model, directly commercially Matching installation is used, and is controlled and is run by peripheral control unit.
See Fig. 1~4, the working principle of the full SERVO CONTROL draw machining center is as follows:
Firstly, operator is pushed to gyro black assembly corresponding position after filling pipe fitting on unloader 28, pass through revolution group
The cooperation of part and loading assemblies is held down assembly by peripheral control unit control and is processed to needs realizing the feeding push of pipe fitting
Pipe fitting carries out compression controller and controls the first driving cylinder 3 and the second driving cylinder 4 respectively, can make the first screw rod 5 in this way
It is rotated, so that pipe-reduction mold 7 slides on the first lead screw 5, to carry out the draw to pipe fitting end；It is easy to operate fast
Victory, may be implemented draw while pipe fitting, and the specific location of the draw can control contracting by magnetostrictive displacement sensor 15
The range ability of pipe mold 7.
The relatively traditional machine for shrinking of the application has the advantages that
1, the equipment uses full SERVO CONTROL, and X-axis two sides couple the by shaft coupling by servo motor band speed reducer respectively
One lead screw 5 drives pipe-reduction mold 7 to be X to movement, while by magnetostrictive displacement sensor 15, closed-loop control is realized, to reach
To X-axis double end draw synchronous shift, the double end draw simultaneously is realized.
2, X-axis pipe-reduction mold 7 is designed using double-station, and primary feed completes two steps of the pre- draw and the secondary draw, with
Reach a draw molding.
3, the driving of Z axis pressure pressure pipe mould drives the second lead screw 13 to move up and down using servo motor band speed reducer.Simultaneously
Compaction mold is designed using adjustable structure, to realize a wide range of size covering.
4, it is combined using actuating cylinder, realizes whole automatic charging blanking circulation.
It is above-described, the only preferable specific embodiment of the utility model, but the protection scope of the utility model is simultaneously
It is not limited to this, anyone skilled in the art within the technical scope disclosed by the utility model, according to this reality
It is subject to equivalent substitution or change with novel technical solution and its utility model design, should all covers the protection in the utility model
Within the scope of.
Claims (9)
1. a kind of full-automatic draw machining center of full SERVO CONTROL, it is characterized in that: there is fuselage (1), in the middle part of the fuselage (1)
It opens up along its length open slot (2), the open slot (2) both ends are symmetrically arranged the first driving motor (3) and second
Driving motor (4), the first driving motor (3) output end and the second driving motor (4) output end are separately connected first
Thick stick (5)；Pass through thread bush (6) connection pipe-reduction mold (7), the meta position of the pipe-reduction mold (7) on first lead screw (5)
Setting holds down assembly in the middle part of fuselage (1)；Described fuselage (1) side also sets up loading assemblies, under the setting of fuselage (1) other side
Expect component.
2. the full-automatic draw machining center of full SERVO CONTROL according to claim 1, it is characterized in that: described holds down assembly
Including guide post (8), upper pressure seat (9), down pressing seat (10), upper and lower clamping platform (11), upper and lower motor (12) and the second lead screw (13)；Institute
The guide post (8) stated is vertically set on fuselage (1), and guide post (8) upper end is fixed by horizontally disposed clamping platform (11) up and down, institute
The motor up and down (12) stated is vertically set on clamping platform (11) upper end up and down, and second lead screw (13) is vertically plugged in up and down
Motor (12) side, the second lead screw (13) passes through upper and lower clamping platform (11) rear end from top to bottom and fixes upper pressure seat (9), described
Down pressing seat (10) is fixed at the lower section of upper pressure seat (9).
3. the full-automatic draw machining center of full SERVO CONTROL according to claim 2, it is characterized in that: the open slot
(2) two sides are located on fuselage (1) upper surface to be also set up guide rail (14) along its length, the pipe-reduction mold (7) lower end two
Side passes through the first sliding block and is slidably arranged on guide rail (14).
4. the full-automatic draw machining center of full SERVO CONTROL according to claim 3, it is characterized in that: the guide rail (14)
Side be located on fuselage (1) end face magnetostrictive displacement sensor (15) be also fixedly installed.
5. the full-automatic draw machining center of full SERVO CONTROL according to claim 2, it is characterized in that: the loading assemblies
Including crossbeam (16), connector (17), fixed block (18), feeding flat-removing air cyclinder (19) and the first claw (20)；The crossbeam
(16) it is fixed in parallel on guide post (8) up and down, the connector (17) is fixed between crossbeam (16), connector
(17) lower end is fixed by fixed block (18), and the feeding flat-removing air cyclinder (19) is horizontally set on fixed block (18) lower end,
First claw (20) is fixed at the output end of feeding flat-removing air cyclinder (19).
6. the full-automatic draw machining center of full SERVO CONTROL according to claim 2, it is characterized in that: the blanking component
Including fixed beam (21), blanking flat-removing air cyclinder (22), link block (23) and the second claw (24)；The fixed beam (21) is horizontal
It is fixed on guide post (8), described blanking flat-removing air cyclinder (22) level is fixed at fixed beam (21) lower end, and blanking translates gas
Cylinder (22) lower end is fixedly connected block (23), and the second claw (24) are fixedly installed in the link block (23) side.
7. the full-automatic draw machining center of full SERVO CONTROL according to claim 3, it is characterized in that: the down pressing seat
(10) lower end is slidably arranged on guide rail (14) by the second sliding block.
8. the full-automatic draw machining center of full SERVO CONTROL according to claim 5, it is characterized in that: the loading assemblies
Lower section also set up gyro black assembly, the gyro black assembly includes turning motor (25), articulated arm (26) and revolution claw (27)；
The turning motor (25) is fixed on fuselage (1) side wall, and turning motor (25) output end is fixed articulated arm (26), institute
Fixed revolution claw (27) in the end for the articulated arm (26) stated.
9. the full-automatic draw machining center of full SERVO CONTROL according to claim 8, it is characterized in that: the gyro black assembly
Side is located at (1) one middle side part of fuselage and also sets up unloader (28).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821984438.8U CN209465579U (en) | 2018-11-29 | 2018-11-29 | The full-automatic draw machining center of full SERVO CONTROL |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821984438.8U CN209465579U (en) | 2018-11-29 | 2018-11-29 | The full-automatic draw machining center of full SERVO CONTROL |
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| Publication Number | Publication Date |
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| CN209465579U true CN209465579U (en) | 2019-10-08 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201821984438.8U Active CN209465579U (en) | 2018-11-29 | 2018-11-29 | The full-automatic draw machining center of full SERVO CONTROL |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109773064A (en) * | 2018-11-29 | 2019-05-21 | 江苏锐成机械有限公司 | A kind of full-automatic draw machining center of full SERVO CONTROL |
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2018
- 2018-11-29 CN CN201821984438.8U patent/CN209465579U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109773064A (en) * | 2018-11-29 | 2019-05-21 | 江苏锐成机械有限公司 | A kind of full-automatic draw machining center of full SERVO CONTROL |
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